SCIENTIFIC ABSTRACT GUBAR, V.F. - GUBAREV, I.D.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R000617210017-6
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Sequence Number: 17
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

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INT-D 163. (KIRA

KAZAKOV, A.A.~ MEWJiIBDZHSKIY, M.Ya.; GUBARI, V.F.
Dependence of the oxygen content in open-hearth steel on
technological factors. Izv. vys. ucheb. zav.; chern. met.
7 no.11,09-65 064. (MIRA 17s12)

CHOKOV, Boris Pavlovich; ERIK, Aleknandr Borisovich; GUM I V F
red. - P
(Production of wall panels from keramzit-perlite concrete)
Proizvodstvo stenovykh panelei iz keramzitoperlitobetona.
Kiev, Budivellryk, 1965. 54 P, (MIRA 18:8)

KULIKOV V.O.; BORNATSKIY, I.I.; ZARURIN, N.G.; D01'0FVY!::V, G.A.;
KALUZIISKIY, Ye.A.; KAZAKOV, A.A.; KOVAL, R.F.; FO:1?11_"VAJv 11I.K.;
TRETIYAKOV, Ye.V.; TRUHOV, Ye.A.; Prinimali uchastiye: ANDREYEV, V.'T'.;
GORDIYENKO, V.V.; GRINEVI(II, I.P.; GURARI, V.F.; DOUNT-11KO, V.I.;
ZHERNOVSKIY, V.S.; 7111GALOVA, Z.1.; KbTiov--g-x-.-.-KURA11.R1 B S.;
OLESHKEVICH.9 T.I.; PRIKH07ffENKO, Ye.
Mastering the operations of 650- and 900-ton (mega - gram) capaci-ty
open-hearth furnaces at the Illich metallurgical plant. Stall 25
no.8:805-807 S 165. (MIRA 18:9)
1. DONNINFIERME-T i Zhdanovskiy metallurgicheskiy zavod imeni Illicha.

113 1

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GUBARI, Y.L.
Injurious effect of alcohol on the stomach. Top.pit. 14 no.2:3-8
Xr-Ap '55. (HLRA 8:6)
1. rz Instituta pitantya AMR SSSR, Moskva.
(ALCOHOL. ITIML, injurious effects,
on stomach)
(STOMACH diseases
alcoh;l lesions$

GUBARI. Y.L.
'!U
Method of isolating a segment of a large Intestine. Flsiol.shur.
41 no.4:587-589 Jl-Ag 155. (NLRA 8:10)
1. Otdol lechobnogo pitanlya InstItuts pitanlya AKK SM, Labo-
ratorlya fisiologit I patologil pishchwarenlya, Moskva*
(INMMNB, LARS, surgery,
isolation for exper. Investigation In animals)

GUBAR V. L.
Collection of urine from animals in long-term experimental studies
(sith al-nary in English]. Fiziol.zhur. U2 no.31:995-997 N 156.
(MIJU 10:1)
1. laboratorlya fiziologit i patologil pishchovarenlya Male
lechabnogo pitadya Instituta pitaniya AKK SSSR, Koskva.
(URINE,
collection in aninals in exper. studies (Rus))

GUBARI, V.L.
Current state of the problem of experimental gastritis. Vop.pit. 21
no.3:72-79 MY-Je 162. (MIRA 15:10)
1. Iz kliniko-fiziologicheskoy laboratorii (zav. - doktor med.nauk
V.L.Gubarl) Instituta pitaniya AMN SSSR, Moskva.
(STOMACH--INFIAMMATION)

22(l) SOV/47-59-2-16/171
AUTHORS: Rozhkov, M.M. (Penza); Starikov, P.A., Engineer (Khabarovsk);
Klenov, A. (Sverdlovsk); Gubarl, V.V.(Elektrostall), and
Malyy, E.L., Senior Engineer,-__-
TITLE: The Movie Projector "Shkollnik" (0 kinoapparaLe "Shkollnik")
PERIODICAL: Fizika v shkole, 1959, Nr 2, pp 68-70 (USSR)
ABSTRACT: The "Kinap" Plants (motion ptcture equipment) in Kiyev and
Leningrad are at present turning out portable film projectors
KPSh-1. They are designed for introducing teaching proces-
ses in schools and demonstrating silent and sound films.
The author lists a number of features which the film projectors
ought to have, such as small weight and size, reliability
and simplicity of op~_ration, fire-proofness, the possibility
to change the moving speed of silent films, to move them
forward and backward, etc. The film projector KPSh-1 has
these features only to a certain extent. The author examines
each of them and points out the shortcomings. The disad-
vantages are also listed by P.A. Starikov, whose school
Card 1/2 acquired the film projector "Shkollnik". A. Klenov (68-ya

The It'lovie Projector ""hkollnik" SOV/47-59-2-16/31
srednyaya shkola - Secondary School Nr 66 in Sverdlovsk),
and V.V. Gubar,' (Secondary Sehool Nr 10 in Elektrostall,
Moscow Oblast ) complain that the projection tubes burned
out and that new ones are not available in the Glavsnabpros
shops. E,L. Malyy, Senior Engineer of the Film Section
of Glavsnabpros, explains why the tubes burned oul too quick-
ly, stating that measures have been taken to supply the shops
with the renuired tubes.
Card 2/2

I" U, E:,. R 1 7 . V .
USSR/1,11edicine - Mosquitoes Bird Nests IkV/ Jun 49
"Bird Nests as Breeding Grounds for Mosouitoes (Phlebotomus)t" P. A. Petrishcheva,
V.- V. Gubarmp A. T. Voylocknikov, I. M. Grokhovskaya, K. It. Sokolva, 0. Ya. Khodova,
A.B. Gasparova, Div of Parasitol and Mled Zool, 1"st of Eridemiol and Iticrobiol,
Acad Med Sci USSR, 2-2' PP
"Zool Zhur" No 3
Investigated 113 nests of nine species of birds and found only eieht contained
evidence of mosquitoes. In these eight nests found eight larva, 25 pupa, md 136 Fum
cases, indicsting that nests are not one of more frequently used breeding places.
Dir, Viv of Parasitol and Med Zool: Acad Ye. 11. Favlovskiy. Dir, Inst of Epideniol
and Microbiol: Prof V. D. Timakov.
FA 151T55

GUDAR 1 2V. V.
USSR/kedicine - Insects, Infectious
Diseases
11, t~"kc , -3
Jun 49
"On the Brooding of Phlebotomus it Colonies of Rhombmys oplaus Licht.#" P. A.
Petriabehova, V. V. Gubarl, Dept Paresitol and Mod Zool, Inst EpIdemiol and Microbiol,
Aced Mod Sci USSR, Moscow
*Entowl Oboz* Vol XXX, No Av Pp 242-245
Various pbases of Phlebotomus papatanii Scop.1, Ph. eergenti Parr., Ph. sergentii var.
almmndri Sint.,, Ph. minutus var. arpklensis Perf., perf., Ph. caucasicus Marzop and
Ph. chinensis Newat. were detect ' Im subterranean dwellings of the rodent Rhombomys
opimus Licht. in vicinity of Yam-kt.- 4n Southwestern Kopetdag.
PA 176T68

I, Ye. G.
GUBt,R', Ye. G.: "Dyna-mic systems on a surface with a small parameter in one of tile
d6rivatives". Minsk, 1955. Min Higher Educniion US:111. Belorussian State U, imenj
V. 1. Lenin. (Dissertations for the Degree of Candidate of Pii.Ysicomathematical
Sciences.)
So: Knizhnaya letouls' No. 49, 3 Decomter 1955. Moscow.

PH-- I BOOK UPWITATION 3OV/2660

VG*SOYU=Iyy matemAtIchookly o'yvzd. 3rd, Moscow, 1956

Tr%kdy. t. 4: Kratkuys, soderzh&n1ye taktalonnykh dokl&doy. Doklady
tw*trwulykh uchanyUM (Transactions or the 3rd All-UnIon KatheSA-
tic4I Conference in Moscow. vol. 4: Summary of 3ectlanal Reports.
S"QrtS of Pbrotgn Scientists) Moscow, Xzd-vO AN SSSR, 2959.
24T P. 2.200 copies printed.
Sponsoring Agency: Abad*miya nauk 333R. MatematicheakiY InstItut. TP

ftdb. Id.t. G.M. Shavchw2ko; ltditorial board: A.A. Abramov. V.0.
BoltYmnskly. A.M. V&slllyev, a.V. Madvedtv, A.D. Myshkis, S.N.
6--1
yLkol-skly (ROOP. 94.), A.0. Postnikov, Yu. V. Prokhorov. ".
ft*W&ovo F. L. U2ty&wvv V.A. Usponsklyo N.G. Chatayov, 0. Yo.
ShIlow, and A.Z. Shumnov.
FUMF=2 This bo~)k Is intended for mathematicians and physIctsts.
00"M&U: 11w book Is Volume rV of the Transactions of the Third All-
union N&tm"tical Confe I hold In Juno and July 1956. The
ranc&
book is dIiTd&-dLatZ- -tw~-~Ln parts. The first part contains sum-
m2r"* Of the Papers Presented by Soviet scientists at the Con-
rWr8%c~ that were hot Included In the first two. volumes. The
second Part contains the text or reports submitted to the edlt*
zi-
by dOn-SovIet Scientists. Zn those cases when the non-Soviet
Ont&Gt did not submit a copy of his paper to the editor. the title

v
at the paper Is altod and, if the paper was printed in a pro l-u-
.....
volume, referance, to made to the appropriate volume. The
pa
p
both Soviet and t&on-3ovi*t, cover various topics In nu:mber
th
eory,

bra, dif'rorentLal and Integral equAtionso function theory,
=
tIonal analysis, probability theory, topology, mattlematical
PVOTPISW of mechanics and physics, computational mathematics,
Ic9l logic and the foundaclons or nathow-stics, And the
ttletory at matbomatics.
lAob&cb~v4 2~7~soodar). On the generalization of the
-
%~a of linear integral equations of M.S. 98garov, 33
certain rorvoLlas, of the Fred-
'rb-01a method and their application to the problem on the *value-
UOU Of *VrOV Of Approximate, methods or solution of Integral
""time 34
and A.
JrA.-
_
Folotsk). WO Ific tions or the concept at
4 dynamic system an the plane 35
4=fioa). Asymptotic expansions, of t&* solution
IM&Y-

rfe-n
41 r t1al equations In powers of a sx&.U pars-
water at highest A-rlvative 36
'Subtractl= method for the solution
GrIPUMUDEry value and sized problems 36
(Zhdanov). On integral equations with ox-
Powatial notainearities 37
Card 8/34

97-57-9-9/17
AUTHORS: Gubar', Yu. D. and Zhelekhovskiy, V. A- (Engineers).
Porous
------------- Coarsely/Concrete. (Elelctroprogrev
TITLE: lectrical Curing of
krupnoporistogo betona).
PERIODICAL: Beton i Zhelezobeton, 1957, Nr.9. pp. 367-368. (USSR).
ABSTRACT: The Russian climate does not allow concreting during
winter without pre-heating of all materials. Pre-
heating by means of steam involves many difficulties;
experience in using no-fine concrete and electrical
pre-heating was obtained during the'construction of
Karagandinsk GRM-2 (power station). Concreting was
carried out continuously from December to April. The
mean monthly temperature in December was - 11.30, in
January - 15.60, in February - 16.70, and in March
- 7.90. The lowest temperature was - 420. The velocity
of north-west winds reached 12 m/sec. Because of con-
crete porosity, the'formation of steam is rather ex-
haustive during pre-heating, which can result in over-
drying. To obviate this, the maximal temperature for
pre-heating no-fine concrete is lower than that of
dense concrete, and should not exesed 33-3500. The
consumption of electricity per 1 m of no-fine con-
Card 1/4 crete is 20% lower than for dense concrete. The current

Porous
Electrical Curinfr of Coarsely/ Concrete. 97-57-0-3/17
used for pre-heatingwas 66-B9 V. Fir
.,.1 shows the
temperature variation of no-fine concrete during pre-
heating; it shows a continuous rise of 5-70 an hour
in temperature durinp, 5-6 hours. 6ix hours after the
commencement of pre-heating, the temperature reached
the maximum, and further increase in temperature was
prevented by repeatedly switching off the current.
After 14-15 hours of pre-heating, the power was finally
switched off. The cooling down lasted 9-10 hours; that
is, it uas slower than warming up. During this cooling
time, the concrete hardened .3ufficidntly to withstand
low temperatures. The graph in Fig.2 shows the increase
in strength of no-fine concrete Mark 50 during pre-
heating. The period during which the temperature in-
creases corresponds with the period of initial setting.
A sharp increase in the strength of the concrete
occurred during the period of the highest temperature
(shovin on Fig.1 between the limits of the practically
horizontal line). AIn that time the strength of the
concrete reached 60 . of the final strength. Later,
when the temp6rature Alls, the strength increases at
Card 2/4 a slower rate. To avoid freezing during transportation,

Porous
Electrical Curing of Coarsely/ Concrete. 97-57-9-9/17
the concrete mix leaves the mixer at a temperature of
not less0than 18 - 2000. If the temperature is lower
than -15 C, 2% calcium chloride (by weight of cement)
is added. This lowers the freezing point, and in- '
creases the electro-conductivity of the mixture. -~he
graph in Fig.3 represents the pre-heating temperature
of the concrete mix containing calcium chloride addi-
tive. This additive shortens the time of pre-heating
and also the time of hardening. The quality of pre-
heatinE, of concrete depends largely on the shape and
location of the electrodes. At first, steel plates
were used fixed to form-mork, but these proved un-
satisfactory, as the paths of concrete immediately
adjacent to the plates become overheated. Rod-type
electrodes proved to be better, and were made from
the waste of reinforcement steel, 4-6 mm diameter.
The distance between electrodes was 25-27 cm. Fig.4
gives an illustration of a wall built from no-fine
concrete. In using these electrodes no over-heating
of concrete was experienced. Overheating may result
if the temperature reaches 40-420, and this is ob-
viated by switching the current off; the concrete is
Card 3/4 allowed to cool down to 20-260, and the current is

Porous
Electrical Curing of coarsely/concrete. 97-57-9-8/17
then switched on again. Fig.5 shows a house built from
no-fine concrete which had been electrically pre-heated,
It is concluded that no-fine concrete can be used with
efficiency in winter conditions. The temperature o:t
the heated concrete should not reach more than 3500.
667o of the ultimate strenp
There are 5 Figures. th is reached in 23-24 hours.
AVAILABLE: Library of Congress.
1. Concrete-Curing methods 2. Concreting-Weather factors
3. Concrete-Heating
Card 4/4

"k
BRODSKIY, A.M.; GUBARII YU.I.
Green's functioum in the nonlinear field theoi7. Iz-r.vys.uchob,
zav.,- fiz. nq..4171-78 161. . (MMA 14:10)
1. Mookovskiy gosudarBtvemyv universitet imeni MN.Lomonosova.
(Potentials, Theory of) (Field theory)

GUBAR1.9 YU.I.
,
"Linearizing" a nonlinear spinor field equation by way of "fusion"
of fermions into bosons. Izv. vys. ucheb. zav.; fiz. no.5:11fO-146
163. (MIRA 26:12)
1. Vsesoyuznyy mochnyy mashinostroitellnyy inetitut,

KWZ, L.; KISIM, A., inzh.; GUBAR17. A., tekhnik-takhnol.og.
Double-dock millet huller. Mkh.-elev. prom. 24 no,4:16-18 Ap 158.
(Ulu 1115)
1, Upravlenlye mukomollao-krupyanykh i kombikormovAh prodpriyatly
Hinisterstva khleboproduktor SSSR (for Khabe, Kiselev). 2. Voronezh-
skoye oblastnoye upravlenlye khleboproduktor (for Gubarev).
(Grain milling machinery)

bal"MV1,6tic mvtb'~d of P"Ustiom *1 untrix" fall
h. A. Grifilibei, athl
1951. No. 10, 14-15.
Tile Up Of loind-itt type 10011MCC.-I WOMM
%trip., all iUI4 urr covmd with an inoulating 14yet of list%-
INIFUIrlo-vol"pholly voullm.. 141111 lwflwt plAtills ibe Swint 6
,Irwa%nl *fill porokilol m4yrol. followed by INA011 "4"..
04.1ird. Orate's with 3-St"? liNth, immshril, voultni with
Chalk-lucal, 411d "w1hell With RtUIL The print 6 then
I'MIOCII(led III ft plAting b6th Of CUS(h 2M, 11980~ M, 4nd
U1011 2 g./1. or CuSOl 20U. 11#50. 30. and 2-naphlbo6ul-
tonic acid I SJI- and plated as c.d. 0.5-3J) snip./sq. din.
ai~ - temp. Owe every 24 he$. the tornk% me hrmlml
itbasimllbrush. Alice deposition of a 4
the Plate in poliabed and used In a machint foc type-camr."':
PftltmblY with 46 9007 of Sh 18-20. Sn 5, and Ph 73-6%
(in- Ma-400*)- The fmcb. step of oma6ons are dc-
TiW OW diMarin for metting-up the nutrix for Igthr.
cullinit are WWWn. (-., U. Kwoupod

K(ROIIEVY V.N., Inzfi.; TSIRKIN, M.Z... inyh.p, LAVRUSH'INA, N.S.,
KONTOROUGH, LoM., inzh.;_K inzh.; Frirti:mal
uchastiye NELIShTEYN, LoG.
Imulation of bar winding heads of the.stators of hydrogenerators and
-turbogeneratorse Elektrotekhnika 36 no.8:16-18 Ag '65. 18--9)
1. Leningradskiy filial Vsesoyuznogo nauchno-issledovatellskogo in-
stituta elekt,.romekhaniki (for Mellshteyn)O

GTJBAFW, A.q., inzhener.
Novel design of a durable hot-blast damper. Stall 15 no.11:1037-1038
N '55. (MM 9: 1)
l.Makeyevskly metallurgicheekly sawod.
(Blast furnaces)

? : TIM ;~rl."! jj-:-1 !q-111 '1 1! ~- I it- " , .--; -. I
DOBRYNIN, V.P., prof.; OLIMiANSKIY, M.A., akademik, lektor; YELIN, Ye.ya.,
dots.; FATIYMIOV, A.S., prof.; XAMARU.-ANj-_TKACf1ENKO, P.L.,
dots.; CHIZIIEVSKIY, M.G., prof.. lektor; AVDONIN, N.S., prof.,
lektor; ONUCHAK, A.L, dots.; DUNIN, M.S., prof., lektor;SAVZDARG.,
E.E.,, prof.,, lektor; IQUWSM-.SKIYj, N.D.9 dots.,, lektor; AVERIYANOV,
S.F., dots., lektor; POLUBOYARINOV, I.I., dots.; GUBAUV, A.N., red.
izd-va; NAUROV, K.M.j, tekbn. red.
(Textbook on agriculture for party schools]Uchebnoe posobie po s*11-
skomu khoziaistvu dlia partiinykh shkol. Moskva. Pt.l. [crop farm-
ing] Zemledelie. 1958. 397 p. (KUU :L5..:L)
lo Kommuunisticheskaya paAiya Sovetskogo Soyuza. VysshoLya par-
tiymya shkola. 2. Vyssbaya partiynays. shkola pri TSentraltnm ko-
mitete Kommunisticheskoy partii Sovetskogo Soyuza (for Dobryninj
01'shanskiyj Gubarevj Tkaebenka, Chizhevskiy, Avdonin, Onuchak,
Dunins, Savzdarg, Kremenetskiy,, Averlyanov). 3. Vs6sDYuzU8Ya akade-
miya sellskokhozyaystvennykh nauk im. V.I.Ienina (for Ollshanskiy).
4. Vysshaya partiynaya shkola pri TSentrallnom komitete Kommunisti-
cheskoy partii Ukrainy (for Yelin,, Polubo, arinov). 5. Gorlkovskaya
Vysshays. partiynaya shkola (for Fatlyanovi.
(Agriculture)

: : I- ., - - : . F.' x . ~ : ;~; ~~ : - :~ t j ~j ~ I I -. I ,] I , , 1 , , .( I 1 -1 1 , I , I ~ - - i , . I ,
GUBAREV, A.N., assistent
Apparatus for determining aoil moisture under field conditions*
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Makw Wathirt. A r
by the method of
lishoildesow. lor5t. K 4"l Obsev"01 ]wsa., sb-oub repeated bewling, The itime rclkatef t~lldillgs The ala,
q. ClwM' Zessir. IOU, U, tws; terild with,oloool. the fewer cTjwk' 4134
JUbW IS. 147-40110%W1 I brealitt IN actual
1
b
b 3

1
pr
Cf. c. A. Sa. tWWO.-An app. is 4clocrilled in w
vrew. Piereing Ol the 1c,t cf Allot It t as
h attlia of be Opeciaw
can Im sub*ted sitnultallrou-1Y tO r0l'sist-I "i'll' shortened the 6121C lJOVrNSAY
W
f
I
k
f
h
4
C01111t
et
on o
losmon
T
e brnll~
Y
it besdiv4. The radivis of bend c" be adfinted at the "It tests and savc valuro To hich r.pre-sruted motor cbpdy
1
p

heginaligg w that it nemains -%I. thmftbQut the test- huse ham Practical lc,l,. It ,
1 bo t1wrelare, recon"WaLled
Th
i
i
d _4
110
mt
c
tY-
-11!
e that the conditic)ns
Tlwgdvtr &pp. was used to t
of artificial aging be maintained &A
,
max. elongations of the outer larest was 16% Of 11111 ksllth- clustlyalipcoasible. rheipeciinensolartificialsole4ratber
pic proMti. of the specit- did

e a
lo
'
h
With this &P
&dt
Of bends th
dutv tbt 00
F
T
i
i
T
-
e
ft
o
4t
te
ng.
n
lu
f
not change
s
'
e a drdaite change In the appowithm Cd The tatthmi of Coraw-1 is I)v,t for Icoin
r
ist
t
d
es
uc
sinm
o
acmswy to pro
g
a
th. weci Mer Clorwation (up to 2U% Of the telving, although it requires careful mallaterience of expo'
OpOmamm 01 nxiditions
it .. (.it that the
c
Si
i
d
l
h
.
n
ng re
e as
ucc% great
e teAstawe of
ki
y t
Mtb)
breaks rather than caliCklo so- the better 1 SWIM Of M- artificial leather to relocat"I bentling and AmWtwcou*
to repeated tornofing. 1-tallittil tk`9 ek"'Bati"a Increases its feloolency to break eat crack, it is v" wvvs-
astawlt,
.4
a glow did not sNwtcn the ti'lle required for the COmPkitio"a mary that artiticiAl Icather be vulcani I a liter de-
eeling of the
r
h
i
t
ifi
l l
Z
e
es
a
c
, p
STM than fills hitherto N-tri custornar
at Match tests. in irstri a, art
M. 0. Moore
faster la'W" TvLq soon observed. Practical tests with boot
zoo
ago

t:o

logo

AA J. % 0
U it AT 10 is
it it OP e( of 11 Kttlt (foci I IT 0 it it 3 i
t

*1 0 00 00 0 0 0 00 : 00 00 0:0 000 00 0 0 0 00 41 0 a 0 0 4101

XOTELINIKOV..V.N., kand.takhn.nauk; CHENTSOVA. K.I., k9nd.tekhn.nauk;
ZYBIN, Yu.P., doktor tekhn.nauk; KOCH3TKOVA, T.S.; ZAKATOTAL, N.D.,
kand.takhn.nauk;-QU-ARU,.ArG~-.-kand.takha.nauk; SHY SOYA, T.P.,
lush.; TOROBOYATA, A.A., kaud.tekhn.nauk; MIRSKIT, V.I., Lush.;
VISMICH. Ye.A., kand.takhn.nauk; GOLIDSHTRYN, A.Y., Lush.;
KALASHUIXOTA. ?.A.. Lush.; SHMOROVICH, M.L.. kand.takha,sank;
KORWODOV. G.A.. lush.; ZAKHAROT. S,,R., rettessent; NiAGOVESTOT,
B.K.. rateensent: STRONGINA. 0.P.. reteensent; SUMP. M.L. re-
teensent; ZUTNT, T.T., retsensent; KOSAWO N.I., reteensent;
SMOOT, I.S.. retsensent-, RMKK, S.N., retmensent; PZwZN , B.M..
reteensent; TSYNBERG, I.A., retsensent; TURBIN, A.S., retseuxent,
SNIFJOVA, Te.V,, reteensent; BUGOSLAVSKAYA, L.A.. retsensent;
GJMOVA, A.3.,,retsensent; KRAIN, N.M..."teensent; KURVARIDZE.
D.S., red.; PLIKYANNIXOT, M.N.. red.; GRACHITA, A.V., red.; NEDVEWT,
L.Ta., takhn.red,
LShoemalcer's handbook] Spravochmik obuvshchika. Tol.l. Moskva,
Gos,mauchno-tekhn.ind-vo lit-ry po legkol proaWshl. 1958. 540 p.
(MIRA 12:4)
l.Gosudarstvennsys Ordena Leains i Ordena Tradovogo Krasnogo 2namni
obaynays fabrika nSkorokhod" imeni Ya.Xalinima (for Zakharov. Blago-
vestov, Strongina, Simldt, Zuyevg Kosarev, Stepanov,'Rame I%VSrAr,
Veynbergg Turbin, Salruova. Bugoslavskaya. 0amova. Xhanim).
(Shoe manuf acture)

28-58-1-9/34
AUTHORS: Zakatova, N.D., and Gubarev, A.S., Candidates of Technical
Sciences, and KhomenR-o-v-a-,-N-.G.-,--Ugineer
TITLE: A New System of Sampling Chrome Leather (Novaya skhema ot-
bora prob khromovykh kozh)
PERIODICALs Standartizatsiya, 19589 # 1, pp 29-30 (USSR)
ABSTRACTs The article describes a new system of sampling chrome
leather, developed by the Tsentral'nyy nauchno-isaledovatell-
skiy institut khozhevenno-obuvnoy promyshlennosti (Central
Scientific Research Institute of the Leather-and-Shoe In-
dustry). The new system consists in using a slightly smal-
ler size of samples, as shown in the illustration (Figure 1).
Tests at 6 different plants showed, that this system re-
duces waste and gives a more correct evaluation of smaller
hides. The article includes a chart showing test results.
A corresponding amendment is suggested for the "GOST 938-45"-
standard.
Card 1/2 There are 2 figures and 1 chart,

A New System of Sampling Chrome Leather 28-58-1-9/34
I ASSOCIATION: TsentralInyy nauchno-issledovatellskiy inatitut kozhevenno-
obuvnoy promyshlennosti (Central Scientific Research In-
stitute of Leather-and-Shoe Industry)
AVAILABLEs Library of Congress
Card 2/2

VOY7SEKHOVSKXY.. V.L.; SHUXENINA, 14.A.j FMROVA, I.M.; ZAKATOVA? N.D.;
GU 97,_A.S.
Determining the ehamical and physiccmechanical indices of Rusnian
leather* Sauch.-isel.trudy TSPIO no.3207-71 160.
(MIM 15312)
(leather-Testing)

SOV/124-57-5-5437
Translation from: Referativnyy zhurnal. Mekhanika, 1957, Nr 5, p 48 (USSR)
AUTHOR: Gubarev, A. V.
TITLE: An Investigation of Narrow Impulse-type Turbine Cascades (Issledo-
vaniye korotkikh aktivnykh turbinnykh reshetok)
PERI ODICAL: Sb. statey nauch. stud. o-va, Mosk. energ. in-t, 1955, Nr 8,
pp 20-40
ABSTRACT: Results are given of an experimental investigation made of the end
losses that occur in turbine-blade cascades exposed to a subsonic
flow. The author examines the influence exerted by s ,ch factors as
blade overlapping, the entrance angle, and the radial length of the
blades. Included is a diagram designed to facilitate analysis of
experimental data. There are typographical errors: in the paper.
Bibliography: 10 references.
N. A. Kolokolltsov
Card 1/i

AID P - 4377
Subject USSR/Power Engineering
Card 1/1 Pub. 110 a - 3/17
Authors : Deych, M. E., V. V. Frolov, Kand. Tech. Sci., and A. V.
Gubarev, Eng., Moscow Power Institute
Title : Research on new shapes of cascades and pressure stages
in turbines.
Periodical : Teploenergetika, 5, 13-22, MY 1956
Abstract : Experiments with a series of bladings of new shapes
including research at supersonic velocity, are described.
Basic aerodynamic data of new blading are given. Ma-
thematical analyzes of various control and pressure
stages designs are presented. Twelve- figures, 6 tables..
Institution : *me
Submitted : No date

GU3,AR-U, I.V., C-nd Trcii 1%ltirlF "Wearw 'v,
1" (Yin cf
a3laxo- turbiner, nt hi(~Ii ,'Uss, 1".".
c:~tjuji U,JSH. Lot; Ccdlor cf L(Ij,.ill flo-~;tir !.Xwill
(K-L, 26---?58, 109)

GUBARBY, A.V..- METCH, X.Te.
~,,
Certain features of a supersonic flow In active cascades. Nauch.
dokl. vys. shkoly; energ. no.2:163-170 158. (KIRA 11:11)
(Cascades (Fluid dynamics))

AUMORS Dey,,t, U.*:~.t~.'.-:m.7s.-t,,~~~-.,-.,,' 'nli~! 1,W-,',6
A..
TITLEs Ths of vey-king b1se-s of lfictf;vs?s tt h4h NP-el.
lea la-dovuk!, x 0 o-!eh -,Ah, re-eh~lok -r~ -
v

ABSTUCTS Ae thtea are no C4 d+rf~1.Ax,-,ctg lljtj,~Pg
for JA-ffjapm#,~,~- gryqat
ijapox t &D ~, F. .4.-c In-ist ljs M-4i ehar3p
&.3 and ~&!-k Arl+t ta,,~ aho-,,OLd oL.IY b4,t,,
-,-cLrvr.tvv ~., ~o &,wqw-, a+,abil-?, f1ov )*s, thl~ wo;_,A".,F~ hied4s
il ,a ma._-Lr3.iar* to jwr,3r*, on V~,- bss:k patille..
fte way 0 doimg i* 14o, pvogfll,~ Ohi bic!k of Ohji 1,1&ds in st,,lA a
iV xtt~SAS 4~. -"",I 7;~.p s-Ts ia!,5t,
-c!LN-QA,,% 11-.Iihdstf~ lfp~vuxs of fAA U.'-womrs
mvy- II !,I,*!!+,(J_ .34 q)

Ao mCvt at ~'s4 ris~t-,.oa oi the Ds,~k of tki tlcds
&.3 WMEOI tvt *.6,1 -~v _izmts 0,611, 4~U.,tfi R* a 8?~-4rp thaLgi. of
t~frrs -,_z6 uw ;a r,.v % 1: .1 u s e -I ! u.~~ 1.
javit),od. C~irx, ta- kt tagh -1 j -.-hi
rf t.IXT d&t _. G 1 0 0,? ~ R 7 4. -?,;. ~, at. L a-mr-I OR I
~,6 14 e 01, 1 to i's it j61 t , L a e v ! u T if
Card 3 th 'S eLrvi re v i,.~ -,,)r. of Otspe

The investigation of working bladts of turbinse 96-59-i2-16/18
at high speed.
of compression on a small inlet sectAon of the chsj=s*JL. The iv.Ur-
blade channel should be either expanding (first method.! or c6ztracting-
expanding (second method). The main types of blada profile are
illustrated in Fig.11 Fig.la, shows profile typa A in-44P-ded for sub-
critical speeds of Mach 0.91 Fig.lb. shown profile type B intended
for Mach 0.9 - 1.25; Fig.1c.. illustrates profile typs C using the
method of stepwise retardation, and Fig.ld. shows th6 profile type C
using the direct Jump nothod. Both class C profiles are used for
high supersonio speeds of Mach greater than 1.3. An arti~zlo by Deych
and others in Toploenergetika, 1956, No.5. gave a notattion of blading
and profiles which in adopted h6rt.. Ths p,7ssaure d4"stribution over
profile TR-AB, s4en in Fig.3.., J~v disaimiltr and 0*
differences are dismsel.. CorrespondAv4 jivtr pro.11N TH-2B.,
which As designed to turn the flow through swaller anglos, are
presented An Fig.4. Velocity dintributIon vurvis oTer pxafAls TR-ID
with somewhat different angles, are giver. in Fig.U- It* disvrlb-mtions
,~f Ino--ts over the h*ight of the blading &Te plottcd JIn FAC.6,; and
the merits of tho different bladingo are rump&T6e,. Grapha of profils
losses in group I blades appear in Fig,.7, Tttal lo4s -,=,7e* for
different typ*s of blading are given in ~N*.g,,S. Plots og snpvzoonio
Card 2/3 flow in turbine blading are sketched in Fig..0,, thb d~,!ft-ree.!,v bt-tween

The investigatAon of working blades af tv-rbAn&s SOV/190-58-12-.10/ ).8
at high speed.
the fLow in typs A blades (Fig.9&7~ ead t1-:pa S lhladts !F~g,ft
explained. The distribution of thos fI,CT OU-A.Ilt fimg] *.I Wyl!g. t~q he~,&t
of blading TR-IB is graphed In Fig.10~ 'Mt tvimin&I '~Tvvva, wtd "~.t
Mach numbsr aro related graphi,tally in Fig,1.1~~,
losses diminish rapidly as the Mach nutd.,#,.r iAv Ina
that for Mach uxuabira of 0.9 - ']"0 1414, As zs-4~sairj- t~, -ava Uad&-t of
group A., Blades of then* proftlvj have low lonots av,d alabllv
character jist A-a a ovor a wid4 range of &nglivs ol flow AnItt,, Far Mash.
numbers of 0.9 - 1.25 '.he profiles should ha-i ohs?p :uilv. vdgt-s and
small cu:rvatm-rs of ths beek of ths blads on thp. iu.143 vs-~tAay.: also,
th,&re should preferably be straight sv4ttanA 4M thi r*giou at the inlet
and outlet edges. Profil-so of Crovp B etarnot b4; -used Irr b-Agh suptr-
sonic speed. The wuwez of total losses giwem An Fig.S. in,,~Iud& two
related to Hades of group C d*xigned in wi.oordau.-* with prinixples
explained in the article. Freliminary test resul-ts ba-re shown tha
eorre4tassm of ths basI4 idea and a n&v ssrt*s of b1tding should
accordingly be dtvs.1oped fo;7 high supersonA..) ap4e4s. There are 11.
figures and ivIU2h are
ASSOCIATIONs Moscow Pow4;r InstitmAs (igoako-vakiv Zm-&rg4t.L,ALa*.k'eIy 1-net-It-at)
Card 3/3

86o8i
S/096/60/000/012/004/008
.2 A.20 E194/E484
AUTHORS: DeXch, M.Ye., Doctor of Technical Sciences and
Gubarev, A.V., Candidate of Technical Sciences
- -------------
TITLE: The Question of "Blockinglt of the Delivery Nozzle and
of the Working Blading Profile in a Supersonic Flowl
PERIODICAL: Teploenergetika, 1960, No.12, pp.27-33
TEXT: In investigating turbine bladin f the active type in a
supersonic flow "blocking" of the nozzle occurred tinder --ertain
conditionsi like the similar effect -.,. wind tunnels, it occurs
because the flow capacity of the model under investigation is less
than that of the nozzle. In a wind tunnel the zone of Mach number
in which 12blocking" is observed may be altered by changing the
geometry of the working part of the tunnel but "blocking" in
turbine blades depends only on the geometry of the nozzle and
blading and the "blocking" zone cannot be altered without altering
these. Accordingly, designers of turbine type machines must
determine regions of "blocking" of blading and analyse the
resulting effects. The application of the X hodograph method
to the analysis of "blocking" conditions is first considered,
Card 1/5

86o8l
S/096/60/000/012/004/008
E194/E484
The Question of "Blocking's of the Delivery Nozzle and of the
Working Blacting Profile in a Supersonic Flow
a description of the method is to be found in the book "Technical
Gas Dynamics" by M.Ye.Deych. The continuity equation is written
for the inlet and outlet sections of the blading in the form of
Eq.(1). The equation may be used for graphical determination of
the flow conditions in the blading by writing the axial projection
of the referred flow through the blading, in the form of Eq.(2) and
(3). The hodograph of the vector may then be constructed which is
a transcendental curve in a polar systein of coordinates (X,O),
A typical hodograph Is shown in Fig.2 and the circle corresponding
to X = I divides the plane of the hodograph intt the two regions
of subsonic and supersonic flows. The use of th( X hodograph
method for calculation with subsonic speeds at inlet and outlet
from the blading presents no difficulties. With supersonic
discharge speed the inlet flow parameters cannot 1,e arbitrarily
selected because it is necessary to maintain the .;peed of sound in
the minimum section of the channel between the bLtdes. If this
Card 2/5

86o8i
S/096/60/(oo/012/004/008
E194/E484
The Question of "Blocking" of the Delivery Mozzie and of the
Working Blading Profile in a Supersonic Flow
condition is fulfilled the hodograph method can Le used without
special difficulty for supersonic exit speeds from the blading.
An example is then described with reference to Fig,24 given the
inlet angle of flow to the blading PI and the dimensionless
velocity Xl. With supersonic speeds at inlet to the blading
the analysis and calculation of the f:ow parameters beyond the
blading is much more complicated, If the ittinittIL1111 section of the
channel between the blades is assumed to occur at the exit the
continuity equation for the characteristic sections may be written
in the form of Eq.(4) and (5). It is then shown that supersonic
flow at the inlet to the blading is theoretically possible only
with an expanding nozzle under certain conditions. The occurrence
of possible regions on the hodograph is discussed. The region of
supersonic conditions in which "blocking" may occur is then
considered. To simplify the analysis the case of an expanding
nozzle and supersonic diffuser is considered, see Fig.3, in which
Card 3/5

8601
S/096/60/000/012/004/008
E194/E484
The Question of "Blocking" of the Delivery Nozzle and of tbe
Working Blading Profile in a Super-sonic Flow
the blading is replaced by art equivalent contracting channel.
It is shown that supersonic speeds in front of the blading are only
possible when Erj.(9) is fulfilled, For practical put-poses it is
recommended to construct the X hodograph diagram in the form
shown in Fig.4. The method of constructing and that of using the
diagram are explained. The diagrain may be used to determine the
angle of deflection of flow in the guide vanes and runner blading.
Calculated and experimental curves of the relationship between the
discharge angle of the flow from the runner blading as funstion of
the inlet angle and the speed of discharge are plotted in Fig.5.
Analysis of the system is much more complicated when there is an
axial gap between the guide nozzle and the blading but the method
of calculation may still be used in this case providing that it is
remembered that if the gap is big enough, the flow conditions of the
nozzle depend only on the back--pressure and the conditions of flow
at the inlet to the blading on the pressure drop and the loss
coefficient in the nozzle. A special feature of gas flow in the
Card 4/5

86oft
S/096/60/000/012/00/oO
E194/E484
The Question of "Blocking" of the Delivery Nozzle and of the
Working Blading Profile in a Supersonic Flow
nozzle blading system when there is an axial gap is that the
blading reaction calculated from the flow parameters at the nozzle
section and at the inlet to the blading are --rery different, see
Fig.6. Serious errors may arise if the flow conditions in the
bladIng are calculated froin data relating to the nozzle discharge
position. Special cases of blade "bl-ckingll are then considered
which may arise when the inlet angle of flow is other than that
designed for. When xhe blading is moving relative to the nozzle,
conditions under which blocking may occur are wider and the so-called
condition of "partial blocking" is typical in this case for high
supersonic speeds, this case is explained with reference to the
vector diagram Fig.8. There are 8 figures and 5 So-iet
references.
ASSOCIATION; Moskovskiy energeticheskiy institut
~Moscow Power Engineering Institute)
Card 5/5

I :- I , .. 1- ~ 4~ 1; .1 1 .; - 1 - , -I ! , ! . I . .. I -
GUBAREV, A.V.; KAZENTSEN, F.V., TRO'YANOVSKIY, lix.
"Aerodynamic experiment in machinery construction" tfy i.L.Povk'ri.
Reviewed by A.V. Gubarev, F.V. Kazintsev, B.M. Troianovskii.
Enerpomashinostroenie 6 no.8:44 Ag I(r. Oulu ll~:q)
(Machinery--Aerodynamics)
(Povkh, I.L.)

SflffNDLIN 1. Ye. (Moskva); GUBAREV, A. V. (Mosk7a); KOVBASYUK, V. 1.
(kookva) j PROKUDINj,-V-.-r.-fmlk")
Froblm concern the optluisation of the operation of mpetO--
bydroonude gennAstorm. Isv. AN WSR. Otd. tekh. nauk. &ergo
i avtm, no,6:34-38 N-D 162, (NIM 16: 1)
(Nagastobydroftamics)

S/147/62/000/002/ol4/o2o
B191/B533
AUTHORS; Gubarev A V Filippov, G.A., Lazarev, L.Ya. and
Pandlya, A.D.
TITLE; A method of design and the results of investigations
of a bladeless guiding assembly for radial-axial
turbines
PERIODICAL: Izvestiya vysshikh uchebnykh zavedeniy, Aviatsionnaya
tekhnika, no.2, 1962, 113-123
TEXT: A simplified analysis of the flow rests on the
assumptions of an ideal gas, a uniform distribution of the flow
parameters in the outlet section of the volute, and the flow
parameters at the outlet section of the entry so-cket being constant
in each cross-section of the volute. Analysis of the continuity
equation shows the ratio of the inlet-and outlet velocities in the
volute to be the main parameter which determines the volute
geometry. This ratio (the "acceleration factor") also determines
whether a bladeless assembly is advisable and Nfhen it drops below
0.5, a bladed one is preferable. As the acceleration factor
increases, the radius of the volute decreases. Various relations
Ca-rd 1/2

A method of design and the results ... S/147/62/000/002/0111/020
E191/E535
are derived and illustrated �n graphs between the volute dimensions
and the acceleration factor. The model of a bladeless stator for
a rotor diameter of 130 mm, a rotor width of 12 mm and a flow
angle of 120 at the rotor entry was tested in the laboratory.
Energy losses in 16 cross-sections around the periphery were
measured together with the flow angles and static pressures. The
static pressures were also measured in the entry socke't and along
the mean volute line. Conclusions: the design procedute put
forward nermits the determination of the volitte geometry and the
behaviour of the volute flow under non-design conditions. The flow
exit angle from the blade-less assembly depends on the flow
velocity even at sub-critical heat transfer conditions. The
efficiencies of bladeless and bladed assemblies (with well
developed entry sockets') are equal. The valute.must be accurately
macfiined to avoid distortion of the velocity field at the turbine
inlet. The limits of application of the bladeless stator have not
yet been fully explored. There are 9 figures.
ASSOCIATION: Moskovskiy energeticheskiy institut, Kafedra
Card 2/2 parovykh i gazovykh turbin (Moscow Power Engineering
Institute, Department of Steam and Gas Turbines)
SUBMITTED: November 17, 1961

39785
s/147/62/000/002/013/020
E191/E-535
AUTHOR: Gubarev. A.V.
TITLE: Investigation of rotor blade cascades for turbines at
supersonic velocities
PERIODICAL: Izvestiya vysshikh uchebnykh zavedeniy, Aviatsionnaya
tekhnika, no.2, 1962, 102-112
TEXT: Some results obtained in the Author's dissertation
presented to the Moscow Power Institute in 1958 are reported,
wherein rotor blade cascades were studied at supersonic velocities.
Previously, sharp entry edges were favoured but were later
considered the source of additional losses. Nose shocks arising
ahead of the cascades, belong to one of three groups, namely those
due to flow around the leading edge, those depenaent on the inter-
blade channel(Ilchannel choking") and those due to a deviation of
flow inlet angle. To reduce the intensity of the edge shocks,
the thickness and wedge angle of the edge should be reduced. This
may conflict with the need to prevent choking of the channel. it
is shown that the flow in the entry portion of*the profile should
not be accelerated. This can be achieved by making the back of the
profile in this portion re-entrant or, by an oblique shock arising
Card 1/3

Investigation of rotor b.lade S/147/62/000/002/013/020
"El9l/E535
at the leading-edge. In both cases the inter-blade channel is
made either convergent-divergent or divergent. Supersonic cascades
are usually installed where the volume flow is moderate and the end
losses significant. Deceleration of the flow in the entry portion
is also beneficial froin the point of view of the end losses. About,
30 different cascades distinguished by profile shape, ' relative
pitch, and stagger were tested in a range of Mach Numbers between
0.85 and 1.54. Pressure distributions and total losses are
illustrated in graphs for various cascades, the geometric
narticulars of which are given in a table. Flow patterns obtaineci
by the Schlieren method are shown in a photograph. In one group of
profiles, the thickness and wedge angles of'the inlet and outlet
edges are small and quite extensive sections on the back of the
profile and others near the edges are straight. The curvatures of
the back and the concav6 surface vary 5moothly. Some profiles
constitute slight modifications of this group. Another group of
Ve"r**og n4o ~tm oo"pav# by an ara of a single
radius. The wedge angle of the inlet and outlet edges is zero.
The inlet portion of the inter-blade channel has the minimum
section and the channel diverges gradually. The field of flow
Card 2/3

investigation of rotor blade S/147/62/000/002/013/020
E191/E535
downstream of the cascades was also examined. The general
conclusions lead to recommendations for the design of improved
sections for supersonic velocities. The losses, although reduced
down to half of those in existing sections are still excessive
(13-1%0- It is generally better to design cascades for the lowest
.Mach Number expected in operation. At large supersonic velocitids,
the end losses in cascades as developed in the present invest~iga-
tion are very small so that these cascades should be used for the
inlet stages of turbines. There are 6 figures and 1 table.
ASSOCIATIONz Moskovskiy energeticheskiy institut,
i gazovykh turbin
(Moscow Power Engineering Institute,
Steam and Gas Turbines)
SUBMITTED: October 13, 1961
Card 3/3
Kafedra parovykh
Department of

DUCH M.Ye., doktor tekhn.nauk# prof* IM&LW
,,A.V. kaand.tekhn.nauk;
FILIPPOV G.A., -TS, W
.9 inzh.; VAN CHZI -TSI Wang
New method for profiling theguiding lattices of stages with lov d/.1
ratio. Teploenergetika 9 no.8:42-47 Ag 162. (HIIM 1527)
1. Moskcvaldy energeticheskiy institute
(Turbines)

~ :, ~ g ~ t ., -.: , ', ~ , , I '. , , 1,.,,-:.
DEYCH, M.Ye., daktor tekhn.nauk;-GUBAREV, A.V., kand.tekhn.nauk; LAZAREV,
L.Ya.P inzh.; DZHAGANKAKHAN, A., inzh.
Investigating the new turbine blade cascade nozzle developed
by the Moscow Prder Engineering Institute for supersonic speeds.
Teploenergetika 9 no.10:47-52 0 162. (MIJU 15:9)
1. Moskovskiy enervaticheakiy institut.
7T-urb-ines-Blades) (Nozzles)

5 IF!
L 10017-6.3 OF (n)-2/kM/ZW (k)/bD$A-2/ZS-(v)/t~ (W)-2--A=1AFna1Arw08D1
ESD-3/S9D-f~)-4/Pm-/t/Pz-4/Pti-4/~'ab-4Ai-4-.TJPCC)/AT/WW
ACCESSION.NR: AP3003450 B/0179/63/000/003/0003/1)008
Madin. S. A
AUTHOR: Qu_barev, A. V. (Moscow); Ko bgnLk, V. I (MosOow);
Y
(Moscow);,ep "in, A. let (Moscow); gggXatskiy-, B. Yu (Moscow)
TITLE: Constant-velocity flow of electroconductive in taie channel of
a mic
erator g'
Ps drodyna gen
SOURCE: AN SSSR. Izv. Otdelo tekhn. -nauk. Mekhanika:i, mashinostroyeni~e,
no. 3, 1963, 3-8
TCPIC TAGS: magnetobydrodynsmic~generator, alectrocon&'6tive, ges, moving
plglsw
ABSTRACT: An analyticalAnvestigation. is made under th,~ folio~ang- asMmTtions&
1) the gas is ideal, nonviscous, and nonheat conductive; 2) the' - channel flow, is
quasi-unidimensiona.1; 3) the gas is electrically neutral; 4) 1 the magnitude of
the secondary ragnetic field is negligible' in comparison with that of thb'external
field; 5) the gas conductivity is constant and isotropic; and 6) the eiec'troae
potential difference is constant. Equations determining theimotion of an
Card 1A

L 10017-63
ACCESSION NR: AP3003450
in an NOD generator were established inlaccordance with
electroconductive-gas
I ion of 1961 (Neyringei. . 09timallneya pneratsiya
Neyringer a.investigat
moshchnostil dvizhushcheysya plumoy. Sb. p~rwrodo* "DVizhushdhV&6YV6 pla~jsma,-"
IL, 1961) and expressed in pertinent parameters. Becoune the'solution of these
equations requires an additional condition, it. vase asstmd that the flow of 9"
takes place either with constant electric.efficiency or constantmegnetl.c:gap.
It was found that constant-magnetic-gap generators at pressure p = 0 generate
their net power in proportion tothe magnitucle of local~electric efficiency at
the channel entrance. Constant-electric-efficiency generators require relatively
high local.electric efficienciesslong tietotal channel length to insurd high
internal generator efficiencies. In high-power installations' channels 'with
increasing.magnetic gap are found to be preferable. Ori.g. art. hash 9.
figures and 13 formtdas-
ASSOCIATIM none
SUBMITTED-s 03jhn62 DATZ AGQ: .24.Tul63 ikLt- 00
00 X01W SOV: 003 MHER::
SUB CODE: 001
Card 2/2

! 1 . I - - 7: , -- !,! ..r! 'I --., , - , 1, ., I . I . I

S/114/63/000/002/003/003
E194/E155
AUTHORS: CAubarev. A.V., Candidate of Technical Sciences,
Fillippov, G.A. Engineer,, and Pandlyal A.D.lEnginser)
TLE. A.bladeless guide arrangement for centripetal turbines
~RIODICAL: Energomashinostroyeniye, no.2, 1963, 38-39
..TEXT: Centripetal turbines. which are used to give low
output combined with high efficiency, currently use bladed gu *ide
arrangements which are efficient only with low gas inlet speeds.
Helical bladeless swirlers are simpler and smaller. They are based
:'on the principle of accelerating the gas in a centripetal swirl by
tangential delivery of the gas to the spiral casing ("scroll").
In designing this arrangement it is necessary to calculate the
section of the spiral at a number of positions. Non-viscouz
uni-dimensional flow is assumed. The following design formulas
are deriveds
JL ~2 4p
qj F q, Ir d sin C1 (5)
2a%
Card 1/2

--- - ------
s/il4/63/000/002/003/003
A blad*less guide arrangement
E194/EI55
d
I
X r a
2
wheret. q quantity of gas; F cross-sectional area of spiral;
d - discharge diameter; height; a - discharge angle. The
suffix 1 relates to discharge conditions; the suffix y t
conditions at an angle V from inlet. Tests were made on guide
equipment designed to these formulas with a discharge diameter of
0
;-130 mm and height of 12 mm with al = 12 Losses were plotted
for a number of sections and varied considerably over the height
of the guide equipment, particularly at low gas speeds. Dischargw
angles also varied. -However, the losses were no greater than in
a bladed guide equipment, and bladeless equipment should be used
.11-because it is smaller, lighter and easier to make. The design
formulas recommended are accurate enough for practical purposes
~,Some of the variations in discharge angle probably resulted from
.manufacturing errors in spiral dimensions.
~:,There are 5 figures.
Card 2/2

L 19884r63 -4' WW
~ACCESSICN NAS AP3004753 S/0096/63/ODO/008/0024/0028
:AUTHORS: G barev (Candidate of technical sciences);
As Ye aim 1-*Pzt -la-mrsy
Yet. (Eng ears)
ITTTLE: ~Effect of wdt edge thickness an ch6raoterlatics of turbdue guide lattices
;SOURCEt Toploenergatika, no. St 196~j 24-28*
TOPI 0 TAGS: turbines guide vane, blade, lattice profiles profile lose
~ABSTRACTs A detailed investigation has been made of the s3dt edge*thickneaq offset
on turbinelcharecteriBtics for mach numbers 0.2-IeZ, Variation In thickness is
-achieved by changing the contour of the profile only on the edwave Bias of the
;vane 4see Enclosure 1). The selected lattice-is type TS-1A with wdt edge thick-
ness of I mm. The pressure distribution on the lattice profiles is obtained for
7various values of blrde pitch T, edge thickness A 1, and mach number3*(,866 EnCIOMMO
2). The effect of exit edge thi'ckness was studied on lattice profile losses, on
end losses, and on totfil turbine efficiency loss. Changng the thickness on the
concave sidebut leaving the effective exit velocity angle and.lattice width con-
stant, induces a significant decrease in profile losses with an increase In the
magnitude of A On thd other hand,,.at large mach numbers, a critical increase in
Card

lo 19884~!63
ACCESSICK SRI 23M4759
12attice 169s was observed when Increasing the e3dt edge t1dohmess. WC. art, has I
17 figures and 1 table.
MOCIATIMs . Abskovskir snergeticheskiy inistitut (Institato- of Power Indnewingl
SIUB17TTEPt 00 DATE AC'qt 3DAug63 IRMI 02
MM COMI Im NO pff SOVI 005 OWRt 001
6ord '21,8 9

GUBAREV, A.V... kand.tekhn.nauk; LI TSAY-SYU [Li TS'ai-hsiu]
Effect of the nonuniformity of the flow on the characteristics ot
the cascades. Teploenergetika 10 no.6:46-48 Je 163. (MIRA 16:7)
1. Moskovskiy energeticheskiy institut.
(Turbines)

---GU.BAREVP A,V.0 kand. tekhn. nauk; SYAN I-MIN [11siang I-ming], inzh.;
LAZAREV, L.Ya., inzh.
Effect of the thickness of the outflow edges on Uie characteristics
of turbine guide blading. Teploenergetika 10 no.8:24-28 Ag 163.
0 (MIM 16 s 8)
1. Maskovskiy energeticheekly institut.
(Turbines)

1 1: - I e ", r I ~!' W I I ~ 6. f, .11 ~ I I I I I I- I . I I I I I . I . I I .
GUBAREV, A,V.9 kand. tekhn. nauk
00
Problems concerning a magnetohydrodynamic method for converting
thermal energy to electric power. Teploenergetika 10 no.9t
81-85 S 163. (MIRA 16ilO)
(Magnetohydrodynamics)
(Thermoelectric generators)

-77
APCESSION NR-. AP4036429 S/0294/64/002/002/0156/0159
iAUTHOR: 9-A. Covbasyuk, V. 1.
-rrr : 'Analysis of the Hall effect In a moving plasma
SOU1=: Teplofizika vy*sddJch temperatur, v. 2, no. 2, 19640 IS6-lSg
TOPIC TAGS: Hall effectq plasma energy balancep graphic computation#
optimal plasma flow
ABSTRAM By representing the electric field vector and the aammt density in
the plasm as complex numbers, so that the power absorbed from the electric exter-
nal field or given up to the field can be plotted as a family of circles in the
emplex planes the authors develop a graphic method for determining the so bal-
ance of a plasm moving in crossed electric and magietic ftelds. Ihe cases consi-
dered are zero longitudinal field, zero transverse fieldv zero longitudinal curr-
ent, and electric field equipotentials making a fixed angle with the pLvm Velo-
city vector. It is pointed out that the graphical tedmique makes it very easy to
determine the optimal plasma flow conditions (when the maxmn energy trwwfer
oocurs at mbdma dissipation)# Orig. arto has: 4 figures and 6 forwolme
Irv 1/2

71
ACCESSION UR: AP4038429
1!,,MOM=ON: Naudm-issledovatalvskiy imtitut vy*~*Al& tempa-atw (sclu*ific
Pasearch botitute of Hio 7fterstum)
SUMMED: l2Nov63 ATD PREM i075 ENC161 00
SM MCEJ Nve M MR Mr SOV: 000 orml 004

GUBARE-11J. A.V.9 kand. tekhn. nauk
FeaLures of a magnetohydrodynauLic method for convertLng heat into
electrical energy. Energ. stroi. no.41:69-77 164., (MIRA 17-.11)

L 06565-67 OWT (1)/EWT(m)_ WP(c) AT/DJ
ACC NR, AP602976i----- SOURCE CODE: UR/029h/66/004/004/0562/0571
AUTHOR: Breyev, V. V.,(Moscow); Gubarev, A. V. (Moscow)
iORG: None
LE: Optimizing flow and load conditions in magnetohydrodynamic generators [Paper
sented at the International Symposium on Magnetohydrodynamic Electric Power Genera-
n, Paris, July 1967~1
: Teplofizika vysokikh temperatur, v. 4, no. h, 1966, 562-571
rOPIC TAGS: MHD generator, electric generator, MHD conference
t;- I
MTRACT: A general formulation is given\for the problem of optimizing the working
characteristics of a magnetohydrodynamic generator used as a power plant. A number of
ci~teria are derived for evaluating the feasibility of using installations with MHD ,f
generators and theoretical numerical data are given on the output characteristics of "
t4e generators and of the installations as a whole. Analysis of the problem of select-
i~g optimum conditions for operation of this type of generator shows that there are a
number of specific characteristics in setting up this type of problem since the M gene.-
erator is a combination of thermal and electric machines where the working fluiddacts
as the "power winding" of the electric generator. In selecting the optimum generator
parameters for power installations, consideration must be given to the thermodynamic
4

L o6565-67
kCCNRt AP6029781
haracteristics of the cycle and to power consummed in driving the compressor and exci.
ation of the magnetic field. It is found that the internal efficiency of the process
n the MRD generator cannot be used as a criterion for the ideality of the operating
ycle for the installation since a reduction in this parameter reduces the overall di-
ensions of the generator as an electric machine with a simultaneous reduction in a
umber of losses (heat losses, power consummed in field excitation, etc.). The optimum
ate of flow for the case where Mopt